D-436T1
The engine is intended to power short- and medium-range regional airlines and other highly efficient passenger and transport aircraft.
The engine meets both current and future requirements of ICAO standards for aircraft engines in terms of noise and emissions.
Take-off thrust is 7,500 kgf. |
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Main advantages of the engine:
- Low specific fuel consumption and low weight-to-thrust ratio;
- High reliability due to long experience in operating the D-36 engine of similar class;
- Low levels of emission and noise;
- Easy maintenance and high effectivity of monitoring and diagnostic system;
- Universal mount for installing the engine on various airplanes in underwing or overwing, fuselage or side positions without changing the engine design;
- Low operating costs at long service life.
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Basic specifications:
| Takeoff power (SLS, ISA +15 °C) |
| Thrust, kgf (kN) |
7,500 (73.55) |
| SFC, kg/kgf•h (kg/kN•h) |
0.370 (37.72) |
| Maximum cruise power (H=11,000,m, M=0.75, ISA) |
| Thrust, kgf (kN) |
1,500 (14.71) |
| SFC, kg/kgf•h (kg/kN•h) |
0.608 (61.97) |
| Dry weight, kg |
1,450 |
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